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MAST flight system dynamic performanceThe MAST Flight System as a test bed for large space structure control algorithms is discussed. An overview is given of the control system architecture. The actuators, the sensors, the control computer, and the baseline damping algorithm are discussed.
Document ID
19870006599
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Davis, L. (NASA Langley Research Center Hampton, VA, United States)
Hyland, D. (NASA Langley Research Center Hampton, VA, United States)
Otten, T. (NASA Langley Research Center Hampton, VA, United States)
Ham, F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1986
Publication Information
Publication: NASA(DOD Control)Structures Interaction Technology, 1986
Subject Category
Structural Mechanics
Accession Number
87N16032
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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